CAP Ascent Abort Aero Presentation for JAXA
2012
41 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Ascent , Aborted missions , Aerodynamics , Aerothermodynamics , Computational fluid dynamics , Crew exploration vehicle , Wind tunnel tests , Launch vehicle configurations , Pitching moments , Data bases , Plumes , Stability , Pressure sensitive paints , Discretization(Mathematics)
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